Negative electrode plate and secondary battery comprising the same

ABSTRACT

The disclosure relates to a secondary battery comprising a negative electrode plate the same. Specifically, the present disclosure provides secondary battery, comprising a negative electrode plate, the negative electrode plate comprises a negative electrode current collector and a negative electrode layer coated on at least one surface of the negative electrode current collector, the negative electrode layer comprising a negative electrode active material, wherein the negative electrode active material comprises a graphite material, and the negative electrode layer fulfills the condition: 0.75≤7.8/D50+1.9*D50/(V OI ) 2 ≤2.0, wherein D50 represents a volume distribution average particle diameter of particles of the negative electrode active material in micron; V OI  represents the OI value of the negative electrode layer. The secondary battery has the combination of high energy density, fast charge, and long cycle life.

CROSS-REFERENCE TO RELATED APPLICATION

This application is a divisional application of U.S. patent applicationU.S. Ser. No. 16/199,246, filed on Nov. 26, 2018, which claims priorityto Chinese Patent Application No. 201810453001.X, filed on May 11, 2018.The aforementioned patent applications are hereby incorporated byreference in their entirety.

TECHNICAL FIELD

The disclosure belongs to the field of electrochemical technology. Moreparticularly, the disclosure refers to a negative electrode plate for asecondary battery and the secondary battery.

BACKGROUND

New energy vehicles represent the direction of industrial development ofthe world's vehicles. As a new rechargeable battery having high-voltageand high energy density, secondary battery has prominent features suchas light weight, high energy density, no pollution, no memory effect,and long service life and thus is widely used in new energy vehicles.

Nevertheless, relatively long charging time is one of the importantfactors that limit the rapid popularization of new energy vehicles. Somepower batteries with fast charge capability have been proposed in theart. However, some of these batteries provide fast charge capability bysacrificing the service life of the batteries. Such kinds of batteriesare obviously not practical. Some manufacturers have introduced newenergy vehicles with fast charge capability. However, most of themsacrifice the energy density of batteries to ensure the fast chargecapability, while the reduced energy density of batteries will shortenthe cruising range of vehicles. Therefore, a secondary battery havingfast charge capability and meanwhile having high energy density isurgently needed in the vehicle field.

SUMMARY

In view of the problems in the art, it is an object of the presentinvention to provide a negative electrode plate and a secondary batterycontaining the negative electrode plate, wherein the battery can haveboth high energy density and fast charge capability.

In order to achieve the above object, the first aspect of the presentdisclosure provides a negative electrode plate, comprising a negativeelectrode current collector and a negative electrode layer coated on atleast one surface of the negative electrode current collector, thenegative electrode layer comprising negative electrode active material,wherein the negative electrode active material comprise graphitematerial, and the negative electrode layer fulfills the condition:0.45≤7.8/D50+1.9×D50/(V _(OI))²≤3.1  formula I)preferably, 0.75≤7.8/D50+1.9×D50/(V _(OI))²≤2.0  formula II)whereinD50 represents a volume distribution average particle diameter ofparticles of the negative electrode active material in micron;V_(OI) represents the OI value of the negative electrode layer.

The inventors have further found that the energy density and cycle lifeof the battery are further improved when the negative electrode activematerial further fulfills the condition:5.3≤D50×0.625+G×3≤14.5  formula III)preferably, 6.5≤D50×0.625+G×3≤12  formula IV)whereinD50 represents a volume distribution average particle diameter ofparticles of the negative electrode active material in micron;G represents the degree of graphitization of the negative electrodeactive material.

For convenience, in the present disclosure, a kinetic parameter isdefined as A=7.8/D50+1.9×D50/(V_(OI))², and a energy density parameteris defined as B=D50×0.625+G×3, and the ratio of A/B is defined as thebattery equilibrium constant K. By further studies, the inventors havefound that the overall performance of battery can be further improvedwhen the battery equilibrium constant K is in the range of from 0.055 to0.31. Preferably, K fulfills the condition 0.112≤K≤0.26.

In another aspect, the disclosure also provides a secondary battery,comprising the negative electrode plate according to the first aspect ofthe present disclosure.

DETAILED DESCRIPTION

Negative electrode plate used for a secondary battery such as a lithiumion battery is generally composed of a negative electrode currentcollector and a negative electrode layer coated on at least one surfaceof the negative electrode current collector, wherein the negativeelectrode layer contains a negative electrode active material and anoptional additive.

The electrochemical process that occurs in a negative electrode plateduring charging can be roughly divided into 3 steps:

1) Liquid phase conduction (including liquid phase diffusion andelectromigration) of active ions within the porous negative electrode;

2) Charge exchange of active ions on the surface of negative electrodeactive material;

3) Solid phase conduction of active ions within the particles ofnegative electrode active material.

Through a large number of studies, the inventors have found that certainparameters of negative electrode active material and negative electrodeplate have different influences on the energy density and fast chargeperformance of battery; when an electrode plate (pole piece) isdesigned, if a special design is made for these parameters, there is achance to obtain a secondary battery that has both high energy densityand fast charge characteristics.

Through a large number of experiments, the inventors have found thatwhen a negative electrode active material and a negative electrode layerare designed, the fast charge performance of secondary battery can begreatly improved if average particle diameter (D50, μm) of the negativeelectrode active material and the OI value of the negative electrodelayer (V_(OI), also referred to as orientation index) fulfill a specificcondition. Specifically, the battery can have a significantly improvedkinetic performance and have a fast charge capability, if a negativeelectrode active material and a negative electrode layer are designed tofulfill the condition,0.45≤7.8/D50+1.9×D50/(V _(OI))²≤3.1  formula I).

For convenience, a kinetic parameter A is defined asA=7.8/D50+1.9×D50/(V_(OI))².

The above formula I is summarized by the inventors through a largenumber of experimental studies. The inventors have found, the fastcharge capability of a battery is closely related to the particle sizeof negative electrode active material (which can be characterized byD50) and the active reaction sites in negative electrode layer (whichcan be characterized the OI value V_(OI) of the negative electrodelayer). Generally, the larger the particle size of the negativeelectrode active material, the larger the solid phase conductionresistance of the ions, and the worse the fast charge capability of thebattery. During charging and discharging, the more the active reactionsites in the negative electrode layer, the faster the charge exchange ofions on the surface of the negative electrode active material duringcharging, and the better the fast charge performance of the battery.Based on this, the inventors have found that by skillfully adjusting theparticle size of the negative electrode active material of the batteryand the OI value (V_(OI)) of the negative electrode layer to obtain amatch and a specific relationship between them, the battery can havefast charge capability without causing a deterioration of cycleperformance.

Specifically, the inventors have found, the improved fast chargeperformance can be achieved by controlling the kinetic parameterA=7.8/D50+1.9×D50/(V_(OI))². Here, D50 represents the average particlesize of negative electrode active material, and V_(OI) represents theorientation index (OI value) of negative electrode layer. The inventorshave found that the number of the active reaction sites in the negativeelectrode layer is closely related to the OI value V_(OI) of thenegative electrode layer. Generally, the smaller value of V_(OI) meansthat the negative electrode layer has sufficient end faces that can berapidly intercalated by ions, and also means the more active reactionsites on the surface.

If the kinetic parameter A is too large, there are two possibilities: 1)D50 is too small, the adhesion of the negative electrode layer isrelatively small, powders tend to fall off from layer, the conductanceof electrons is affected, thus the battery kinetic performance will beimpaired; 2) the OI value V_(OI) of the negative electrode layer is toosmall, indicating that the active material tends to be disorderlyarranged, and the adhesion of the negative electrode layer is bad andpowders tend to fall off from layer, the electrode plate tends towrinkle during cycle test, resulting in the deteriorated reactioninterface, so that the cycle performance of the battery is deteriorated.If the kinetic parameter A is too small, there are also twopossibilities: 1) D50 is too large, the solid phase diffusion isdifficult, thus the fast charge function cannot be satisfied; 2) the OIvalue V_(OI) of the negative electrode layer is too large, indicatingthe active material tends to be arranged in parallel to currentcollector, the effective ion-intercalatable end faces on the negativeelectrode layer is less, that is, the number of active reaction sites isrelatively small, the charge exchange rate is affected, thus the demandfor fast charging cannot be met. Therefore, in order to obtain a batteryhaving the fast charge capability, it is necessary to fulfill thecondition of 0.45≤A≤3.1. The inventors have further found that thepreferred range of A is 0.75≤A≤2.0.

The inventors have further found that, under the proviso that thekinetic parameter A fulfills the condition of 0.45≤A≤3.1 (preferably,0.75≤A≤2.0), if the negative electrode active material further fulfillsthe condition:5.3≤D50×0.625+G×3≤14.5  formula III)the secondary battery may have fast charge capability and meanwhile havefurther improved cycle life and energy density, with better processingperformance of plate.

For the sake of convenience, the energy density parameter B is definedas B=D50×0.625+G×3.

The inventors have found: the energy density of the battery is closelyrelated to the particle size of the negative electrode active materialand the degree of graphitization. Usually, the larger the particles ofthe negative electrode active material, the more the activeion-intercalatable sites. That means, the negative electrode activematerial has higher capacity per gram, and only relatively small amountof negative electrode active materials are required to achieve thecapacity target when the battery is designed. Thus, with the largerparticles of the negative electrode active material, the energy densityof the battery would be more favorably increased; the higher degree ofgraphitization of the negative electrode active material means that thecrystal structure is closer to the complete layered structure of theideal graphite, and has fewer defects such as stacking faults anddislocations. That means, if the negative electrode active material hashigher capacity per gram, only relatively small amount of the negativeelectrode active materials are required to achieve the capacity targetwhen the battery is designed. Thus, with the higher degree ofgraphitization of the negative electrode active material, the energydensity of the battery would be more favorably increased. The inventorshave found that, by jointly controlling the particle size and the degreeof graphitization of the negative electrode active material, the energydensity and the cycle performance of the battery can be furtherconsidered and improved. Specifically, it is realized by controlling therange of the energy density parameter B=D50×0.625+G×3.

If the energy density parameter B is too large, there are twopossibilities: 1) D50 is too large, the slurry tends to settle, bumpingis likely to occur during coating with low yield, resulting in worsecycle performance; 2) the degree of graphitization is too large, theparticles tend to be flat, and the structure of pores is too dense,which is not conducive to the infiltration of electrolyte andsignificantly reduces the cycle performance of the battery. If theenergy density parameter B is too small, there are also twopossibilities: 1) D50 is too small, the amount of the activeion-intercalatable sites is relatively low, that means, the negativeelectrode active material has lower capacity per gram and the batteryhas lower energy density; 2) the degree of graphitization G is toosmall, the crystals tend to have amorphous structure with many defects,and the negative electrode active material has lower capacity per gram,which is disadvantageous for designing a battery with high energydensity. Therefore, under comprehensive consideration, B has a range of5.3≤B≤14.5, more preferably 6.5≤B≤12, in which case the cycleperformance, energy density, fast charge performance are excellent.

In the disclosure, the ratio of A/B is defined as a battery equilibriumconstant K. The inventors have further found that, the overallperformance of the battery can be further improved when batteryequilibrium constant K is in the range of from 0.055 to 0.31.

When A is too small or B is too large so that the battery equilibriumconstant K<0.055, the charging speed is sacrificed to obtain a batterywith high energy density, resulting in high risk of reduction andplating (deposition) of active ions at negative electrode, thus thebattery has a great safety hazard and the cycle performance of thebattery cannot be guaranteed.

When A is too large or B is too small so that the battery equilibriumconstant K>0.31, the energy density is sacrificed to obtain a batterywith high charging speed, which will cause troubles in actual use due tothe relatively short cruising range of the battery. Therefore, undercomprehensive consideration, K fulfills the condition of 0.055≤K≤0.31,preferably 0.112≤K≤0.26.

As used herein, in the context related to the negative electrode activematerial, the parameters including average particle diameter D50, thedegree of graphitization G and the orientation index V_(OI) of thenegative electrode layer have the common meanings well known in the art.

D50 is used for characterizing the particle size of the negativeelectrode active material. It physically means the particle diameterwhich corresponds to 50% of the volume distribution of the negativeelectrode active material particles, i.e., the volume distributionaverage particle diameter. D50 can be determined by methods well knownin the art, such as the methods described in the Examples sectionherein.

The degree of graphitization G indicates the degree to which thestructure of the negative electrode active material is close to thecomplete layered structure of the ideal graphite. The degree ofgraphitization G of the negative electrode active material can bedetermined by methods well known in the art, such as the methodsdescribed in the Examples section herein.

The orientation index OI value (i.e. V_(OI)) of the negative electrodelayer represents the degree of anisotropy of crystal grain alignment inthe negative electrode layer. The OI value of the negative electrodelayer can be determined by methods well known in the art, such as themethods described in the Examples section herein.

The negative electrode plate in the present disclosure can be preparedby methods well known in the art. Typically, the negative electrodeactive material is mixed with materials such as optional conductiveagent (such as carbon materials, like carbon black), binder (such asSBR), thickening and dispersing agent (such as CMC) and other optionaladditives (such as PTC thermistor material), and then dispersed insolvent (such as deionized water). Upon uniformly stirring, the mixtureis coated on at least one surface of the negative electrode currentcollector. After drying, a negative electrode plate containing thenegative electrode layer is obtained. Typically, in the preparation ofthe negative electrode plate, a negative electrode coating layer is notformed on a part of current collector, and a part of the remainingcurrent collector is used as the leading wire portion of the negativeelectrode. Certainly, the leading wire portion may also be added later.

As the negative electrode current collector, a material for example ametal foil, such as copper foil, or a porous metal plate can be used.Copper foil having a thickness of 5 to 30 μm is commonly used. Thethickness of the single-layer negative electrode layer on the negativeelectrode current collector is usually from 5 μm to 80 μm.

It should be noted that the OI value of the negative electrode layer inthe present disclosure can be controlled by adjusting the followingparameters.

First, both the average particle diameter D50 of the negative electrodeactive material and the OI value G_(OI) of the active material powderhave a certain influence on the OI value of the negative electrodelayer; the higher the D50 of the negative electrode active material, thehigher the OI value of the negative electrode layer, the higher thepowder OI value of the negative electrode active material, the OI valueof the negative electrode layer.

Second, in the preparation of a battery, the magnetic field inducingtechnology can be introduced in the coating process to artificiallyinduce the arrangement of the negative electrode active material on theelectrode plate, thereby changing the OI value of the negative electrodelayer. The arrangement of the negative electrode active material mayalso be controlled by adjusting the press density of the negativeelectrode layer in the cold pressing step, thereby controlling the OIvalue of the negative electrode layer.

Preferably, the OI value V_(OI) of the negative electrode layer is1.5-100, further preferably 1.5-50.

Preferably, the press density of the negative electrode layer is in therange of 0.8-2.0 g/cm³, further preferably 1.0-1.6 g/cm³.

Preferably, the average particle diameter D50 of the negative electrodeactive material is 3-25 μm, further preferably 4-15 μm.

Preferably, the powder OI value G_(OI) of the negative electrode activematerial is 0.5-7, more preferably 2-4.5.

The negative electrode active material used for the negative electrodeplate according to the disclosure comprises graphite material. Thegraphite material may be selected from at least one of artificialgraphite and natural graphite.

In one embodiment, in addition to graphite material, the negativeelectrode active material may also comprise one or more of soft carbon,hard carbon, carbon fiber, mesocarbon microbead, silicon-based material,tin-based material, lithium titanate.

The silicon-based material may be selected from one or more of elementalsilicon, silicon oxide, silicon carbon composite, silicon alloy. Thetin-based material may be selected from one or more of elemental tin,tin oxide compound, tin alloy

Furthermore, in an embodiment wherein the negative electrode activematerial is a mixture, the graphite material generally constituteshigher than 50%, preferably higher than 60%, 65%, 70%, 75%, 80%, 85%,90%, or 95% by weight of the negative electrode active material.

The negative electrode active materials suitable for use in thedisclosure are commonly used materials for secondary battery known inthe art, and are commercially available. The graphite material underdifferent types supplied by different manufacturers may have varyingaverage particle diameter D50 and the degree of graphitization G. Or,the negative electrode active material having the specific D50 and thedegree of graphitization G as defined by the disclosure may also beproduced by a conventional process for the preparation of negativeelectrode active material in the art (such as, the methods in theExamples section). The present disclosure focuses on selecting aspecific graphite material (and other negative electrode activematerials), and controlling the OI value of the negative electrodelayer, so that the parameters (for example, the average particlediameter D50 or the degree of graphitization G, etc.) of the negativeelectrode active material and the negative electrode layer arereasonably matched with the OI value of the negative electrode layer,thereby achieving the technical effects of the disclosure. Preferably,the degree of graphitization G of graphite material used in thedisclosure is 40%-99%, further preferably 80%-98%.

In another aspect, the present disclosure provides a secondary battery,comprising the negative electrode plate according to the first aspect ofthe disclosure.

Except use of the negative electrode plate of the disclosure, theconstruction and the preparation method of the secondary battery of thedisclosure are well known. Generally, a secondary battery is mainlycomposed of a negative electrode, a positive electrode, a separator, andan electrolyte, wherein the positive and negative electrodes areimmersed in the electrolyte, and the active ions in the electrolyte as amedium are moved between the positive and negative electrodes to realizecharging and discharging of the battery. In order to avoid short circuitbetween the positive and negative electrodes through the electrolyte, itis necessary to separate the positive and negative electrodes with aseparator. The shape of the secondary battery may be, for example, acylindrical shape (square cylinder or cylindrical shape), wherein thesecondary battery may have an aluminum shell as a casing, or may be asoft package battery.

It should be noted that the battery according to another aspect of thepresent application may be a lithium ion battery, a sodium ion battery,and any other battery using the negative electrode plate of the firstaspect of the present disclosure.

Specifically, when the battery is a lithium ion battery:

The positive electrode plate comprises a positive electrode currentcollector and a positive electrode layer disposed on the surface of thepositive electrode current collector, wherein the positive electrodelayer comprises a positive electrode active material, and the positiveelectrode active material may be selected from the group of lithiumcobalt oxide, lithium nickel oxide, lithium manganese oxide, and lithiumnickel manganese oxide, lithium nickel cobalt manganese oxide, lithiumnickel cobalt aluminum oxide, transition metal phosphate, etc. However,the present application is not limited to these materials, and otherconventionally known materials that can be used as a positive electrodeactive material of a lithium ion battery may also be used. Thesepositive electrode active materials may be used alone or in combinationof two or more.

Specifically, when the battery is a sodium ion battery:

The positive electrode plate comprises a positive electrode currentcollector and a positive electrode layer disposed on the surface of thepositive electrode current collector, wherein the positive electrodelayer comprises a positive electrode active material, and the positiveelectrode active material may be selected from the group of sodium ironcomposite oxide (NaFeO₂), sodium cobalt composite oxide (NaCoO₂), sodiumchromium composite oxide (NaCrO₂), sodium manganese composite oxide(NaMnO₂), sodium nickel composite oxide (NaNiO₂), sodium nickel titaniumcomposite oxide (NaNi_(1/2)Ti_(1/2)O₂), sodium nickel manganesecomposite oxide (NaNi_(1/2)Mn_(1/2)O₂), sodium iron manganese compositeoxide (Na_(2/3)Fe_(1/3)Mn_(2/3)O₂), sodium nickel cobalt manganesecomposite oxide (NaNi_(1/3)Co_(1/3)Mn_(1/3)O₂), sodium iron phosphatecompound (NaFePO₄), sodium manganese phosphate compound (NaMnPO₄),sodium cobalt phosphate compound (NaCoPO₄), Prussian blue materials,polyanionic materials (phosphate, fluorophosphate, pyrophosphate,sulfate) and the like. However, the present application is not limitedto these materials, and other conventionally known materials that can beused as a positive electrode active material of a sodium ion battery mayalso be used. These positive electrode active materials may be usedalone or in combination of two or more.

In the battery of another aspect of the disclosure, the particular typesand the constitution of the separator and the electrolyte are notspecifically limited, and may be selected depending on the actual needs.

Specifically, the separator may be selected from the group consisting ofa polyethylene layer, a polypropylene layer, a polyvinylidene fluoridelayer, and a multilayer composite layer thereof.

Specifically, when the battery is a lithium ion battery, as nonaqueouselectrolyte, a lithium salt solution dissolved in an organic solvent isgenerally used. Lithium salt is an inorganic lithium salt, such asLiClO₄, LiPF₆, LiBF₄, LiAsF₆, LiSbF₆ and the like, or organic lithiumsalt, such as LiCF₃SO₃, LiCF₃CO₂, Li₂C₂F₄(SO₃)₂, LiN(CF₃SO₂)₂,LiC(CF₃SO₂)₃, LiC_(n)F_(2n+1)SO₃(n≥2). The organic solvent used innonaqueous electrolyte is a cyclic carbonate, such as ethylenecarbonate, propylene carbonate, butylene carbonate or vinylene carbonateand the like; a chain-like carbonate, such as dimethyl carbonate,diethyl carbonate or methyl ethyl carbonate and the like; a chain-likeester such as methyl propionate and the like; cyclic ester such asγ-butyrolactone and the like; a chain-like ether, such asdimethoxyethane, diethyl ether, diethylene glycol dimethyl ether, andtriethylene glycol dimethyl ether and the like; a cyclic ether, such astetrahydrofuran, 2-methyltetrahydrofuran and the like; a nitrile, suchas acetonitrile, propionitrile and the like; or a mixture of thesesolvents.

Hereinafter, a lithium ion secondary battery will be used as an examplefor briefly illustrating the structure and preparation method of thesecondary battery of the present disclosure.

First, a battery positive electrode plate is prepared in accordance witha conventional method in the art. The positive electrode active materialused for the positive electrode plate is not limited in the presentdisclosure. Usually, in the above positive electrode active material, itis necessary to add a conductive agent (for example, carbon materials,like carbon black), a binder (for example, PVDF), or the like. Ifneeded, other additives such as PTC thermistor materials and the likemay also be added. These materials are usually mixed and dispersed in asolvent (for example, NMP), and after uniformly stirring, the mixture isuniformly coated on a positive electrode current collector, and dried toobtain a positive electrode plate. As the positive electrode currentcollector, a material for example a metal foil, such as aluminum foil,or a porous metal plate can be used. Aluminum foil having a thickness of8 to 30 μm is commonly used. The thickness of coating (layer) on thepositive electrode current collector is usually from 5 μm to 60 μm.Typically, in the preparation of the positive electrode plate, apositive electrode coating layer is not formed on a part of currentcollector, and a part of the remaining current collector is used as theleading wire portion of the positive electrode. Certainly, the leadingwire portion may also be added later.

Then, the negative electrode plate of the present disclosure is preparedas described above.

Finally, the positive electrode plate, the separator, the negativeelectrode plate are stacked in order, so that the separator ispositioned between the positive and the negative electrode plates forthe purpose of separation, then wound to obtain a bare battery cell. Thebare battery cell is placed in the outside casing, and dried. Then theelectrolyte is injected. After vacuum encapsulation, standing,formation, shaping, and the like, a secondary battery is obtained.

The present disclosure can allow a secondary battery having an excellentfast charge capability as compared with the conventional negativeelectrode plate. Through further optimization, the energy density, cycleperformance, and safety performance of the battery can be simultaneouslyconsidered and improved. Therefore, it is of great significance for thefields of such as new energy vehicles.

Advantageous effects of the present invention will be further describedbelow in conjunction with the examples.

Examples

In order to make the objects, the technical solutions and the beneficialtechnical effects of the present disclosure more clear, the presentdisclosure will be further described in details with reference to theexamples below. However, it is to be understood that the examples of thepresent disclosure are not intended to limit the invention, and theembodiments of the disclosure are not limited to the examples set forthherein. The specific experimental conditions or operating conditions arenot specified in the examples, and the examples are usually preparedaccording to the conditions recommended by the material supplier.

I. Preparation Method of the Negative Electrode Active Material

The graphites having different D50 and G used in Examples 1-49 andComparative Examples 1-6 are commercially available or can be preparedby the following production methods.

(1) Crushing: crushing the precursor (for example pitch coke orpetroleum coke is selected as needed) to obtain a raw material having anaverage particle diameter of 5-20 μm;

(2) Shaping and grading: shaping the raw material obtained in (1),followed by performing a grading treatment to adjust the particle sizedistribution of the raw material (generally, removing particles havingan excessively large particle size and particles having an excessivelysmall particle size);

(3) Granulating: mixing the raw materials and the binder obtained afterthe shaping and sieving in (2) in a certain mass ratio, followed bygranulating (this step can be canceled according to actual situation);

(4) Granulating: graphitizing the raw material after the granulation in(3), for example, in an Acheson graphitization furnace at a temperatureof such as 2800-3250° C.;

(5) Coating and carbonizing: the raw material after the graphitizationin (4) are mixed with a coating agent at a certain mass ratio and thencarbonized, for example, in an orbital kiln at a temperature of such as900 to 1500° C. (this step can be cancelled according to the actualsituation);

(6) Sieving and demagnetizing: sieving and demagnetizing the materialobtained in (5) to obtain a desired negative material.

The average particle diameter D50 of the active material can be adjustedby crushing, shaping and grading, granulating, coating and carbonizingsteps. The degree of graphitization G of the negative electrode activematerial can be adjusted by graphitizing, coating and carbonizing steps.

II. Preparation Method of the Testing Battery

The batteries of Examples 1-49 and Comparative Examples 1-6 wereprepared by the following methods.

A) Preparation Method of the Positive Electrode Plate:

The positive electrode active material NCM523(LiNi_(0.5)Co_(0.2)Mn_(0.3)O₂), a conductive agent (Super P), a binder(PVDF), etc. were mixed at a ratio of 96:2:2. After addition of asolvent (NMP), the mixture was stirred under a vacuum stirrer until thesystem was uniformly transparent, yielding a positive electrode slurry.The positive electrode slurry was uniformly coated on the aluminum foilof the positive electrode current collector. The positive electrodecurrent collector coated with the positive electrode slurry wasair-dried at room temperature, transferred to an oven for drying, andthen subjected to cold pressing and slitting to obtain a positiveelectrode plate.

B) Preparation Method of the Negative Electrode Plate:

The negative electrode active material (graphite or mixed materialcontaining graphite), a conductive agent (Super P), a thickening agent(carboxymethyl cellulose), a binder (SBR), etc. were mixed at a ratio of96.4:1:1.2:1.4. The mixture was uniformly mixed with solvent (deionizedwater) under a vacuum stirrer to prepare a negative electrode slurry.The negative electrode slurry was uniformly coated on the copper foil ofthe negative electrode current collector. The negative electrode currentcollector coated with the negative electrode slurry was air-dried atroom temperature, transferred to an oven for drying, and then subjectedto cold pressing and slitting to obtain a negative electrode plate.

C) Preparation Method of Electrolyte:

Ethylene carbonate (EC), ethyl methyl carbonate (EMC), and diethylcarbonate (DEC) were mixed at a volume ratio of 1:1:1. Then thesufficiently dried lithium salt LiPF₆ was dissolved at a ratio of 1mol/L in a mixed organic solvent, to prepare an electrolyte solution.

D) The Preparation Method of Separator:

A 12 micron polyethylene layer was chosen.

E) Assembly of the Battery:

The positive electrode plate, the separator and the negative electrodeplate were stacked in order, so that the separator is positioned betweenthe positive and negative electrode plates for the purpose ofseparation, and then wound to obtain a bare battery cell. The barebattery cell was placed in the outer casing. The prepared electrolytesolution was injected into the dried bare battery cell. After vacuumencapsulation, standing, formation, shaping, and the like, a lithium ionsecondary battery is obtained.

III. Testing Methods of Performance Parameters

The performance parameters involved in Examples 1-49 and ComparativeExamples 1-6 were measured in the following methods.

1, Testing the Parameters of Negative Electrode Active Material

1) D50: The particle size distribution was measured using a laserdiffraction particle size distribution measuring instrument (Mastersizer3000) according to the laser diffraction method for measuring particlesize distribution in GB/T19077-2016. For the volume distribution, themedian value D50 was used to represent the average particle diameter.

2) G: By using X-ray powder diffractometer (X'pert PRO) according to theX-ray diffraction analysis method and the lattice parameterdetermination method of graphite JIS K 0131-1996, JB/T4220-2011, d₀₀₂was measured. Then, the degree of graphitization G was calculatedaccording to the formula G=(0.344−d₀₀₂)/(0.344−0.3354), where d₀₀₂ isthe layer spacing in the crystal structure of the negative electrodeactive material expressed in nanometer.

2, Testing the Parameters of the Negative Electrode Plate

Testing the OI value V_(OI) of the negative electrode layer: By using anX-ray powder diffractometer (X'pert PRO) according to the X-raydiffraction analysis method and the lattice parameter determinationmethod of graphite JIS K 0131-1996, JB/T4220-2011, X-ray diffractionspectrum was obtained. Then, the OI value of the negative electrodelayer can be calculated according to V_(OI)=C₀₀₄/C₁₁₀, wherein C₀₀₄ wasthe peak area of the 004 characteristic diffraction peak, and C₁₁₀ isthe peak area of the 110 characteristic diffraction peak.

3, Testing the Performance of the Battery

1) Testing Energy Density

The lithium ion batteries prepared in Examples and Comparative Exampleswere fully charged at a 1 C rate and fully charged at a 1 C rate at 25°C., and the actual discharge energy was recorded. The lithium ionbatteries were weighed using an electronic balance at 25° C. The ratioof the actual discharge energy of a lithium ion battery 1C to the weightof a lithium ion battery was the actual energy density of the lithiumion battery.

Wherein: when the actual energy density was less than 80% of the targetenergy density, the actual energy density of the battery was consideredto be very low; when the actual energy density was greater than or equalto 80% of the target energy density and less than 95% of the targetenergy density, the actual energy density of the battery was consideredto be low; when the actual energy density was greater than or equal to95% of the target energy density and less than 105% of the target energydensity, the actual energy density of the battery was considered to bemoderate; when the actual energy density was greater than or equal to105% of the target energy density and less than 120% of the targetenergy density, the actual energy density of the battery was consideredto be high; when the actual energy density was 120% or more of thetarget energy density, the actual energy density of the battery wasconsidered to be very high.

2) Kinetic Performance (Fast Charge Performance)

The lithium ion batteries prepared in Examples and Comparative Exampleswere fully charged at a 4 C rate and fully discharged at a 1 C rate at25° C. This procedure was repeated ten times. Then the lithium ionbatteries were fully charged at a 4 C rate, followed by disassemblingthe negative electrode plate and visually inspecting the lithiumprecipitated on the negative electrode plate. The area of the lithiumprecipitated area of less than 5% was considered to be slight lithiumprecipitation. The area of the lithium precipitated area of 5% to 40%was considered to be moderate lithium precipitation. The area of thelithium precipitated area of greater than 40% was considered to beserious lithium precipitation.

3) Testing Cycle Performance:

At 25° C., the lithium ion batteries prepared in Examples andComparative Examples were charged at a 3 C rate, discharged at a 1 Crate, until the capacity of the lithium ion batteries were attenuated to80% of the initial capacity. The cycle times were recorded.

IV. The Testing Results of Examples and Comparative Examples

The batteries of Examples 1-49 and Comparative Examples 1-6 wereprepared according to the above methods. The performance parameters weremeasured. The results were shown as below.

Negative Particle Degree of OI value Kinetic Energy electrode diametergraphitization V_(OI) of parameter density Items material D50(μm) Glayer A B Example 1 graphite 19 90.00% 5 1.85 14.58 Example 2 graphite19 90.00% 9 0.86 14.58 Example 3 graphite 19 90.00% 10 0.77 14.58Example 4 graphite 19 90.00% 20 0.50 14.58 Example 5 graphite 19 90.00%25 0.47 14.58 Example 6 graphite 19 90.00% 30 0.45 14.58 Example 7graphite 15 90.00% 120 0.52 12.08 Example 8 graphite 15 90.00% 40 0.5412.08 Example 9 graphite 15 90.00% 11.5 0.74 12.08 Example 10 graphite15 90.00% 11 0.76 12.08 Example 11 graphite 15 90.00% 6 1.31 12.08Example 12 graphite 15 90.00% 3.5 2.85 12.08 Example 13 graphite 490.00% 2.6 3.07 5.20 Example 14 graphite 4 90.00% 4.5 2.33 5.20 Example15 graphite 4 90.00% 10 2.03 5.20 Example 16 graphite 4 90.00% 20 1.975.20 Example 17 graphite 4 90.00% 50 1.95 5.20 Example 18 graphite 490.00% 80 1.95 5.20 Example 19 graphite 2.6 90.00% 15 3.02 4.33 Example20 graphite 3 90.00% 15 2.63 4.58 Example 21 graphite 5 90.00% 15 1.605.83 Example 22 graphite 10 90.00% 15 0.86 8.95 Example 23 graphite 1890.00% 15 0.59 13.95 Example 24 graphite 25 90.00% 15 0.52 18.33 Example25 graphite 27 90.00% 15 0.52 19.58 Example 26 graphite 19 70.00% 200.50 13.98 Example 27 graphite 19 80.00% 20 0.50 14.28 Example 28graphite 19 85.00% 20 0.50 14.43 Example 29 graphite 19 95.00% 20 0.5014.73 Example 30 graphite 19 99.00% 20 0.50 14.85 Example 31 graphite 1570.00% 20 0.59 11.48 Example 32 graphite 15 80.00% 20 0.59 11.78 Example33 graphite 15 85.00% 20 0.59 11.93 Example 34 graphite 15 95.00% 200.59 12.23 Example 35 graphite 15 99.00% 20 0.59 12.35 Example 36graphite 4 70.00% 20 1.97 4.60 Example 37 graphite 4 80.00% 20 1.97 4.90Example 38 graphite 4 85.00% 20 1.97 5.05 Example 39 graphite 4 95.00%20 1.97 5.35 Example 40 graphite 4 99.00% 20 1.97 5.47 Example 41graphite 5.7 96.00% 5.5 1.73 6.44 Example 42 graphite 6.2 90.00% 4 1.996.58 Example 43 graphite 14 90.00% 6 1.30 11.45 Example 44 graphite 1580.00% 6 1.31 11.78 Example 45 graphite 5 93.00% 5 1.94 5.92 Example 46graphite 7 70.00% 4 1.95 6.48 Example 47 graphite + soft 7 90.00% 121.21 7.08 carbon (7:3) Example 48 graphite + hard 6.5 88.00% 10 1.326.70 carbon (7:3) Example 49 graphite + lithium 7 91.00% 14 1.18 7.11titanate (7:3) Comparative graphite 30 90.00% 40 0.30 21.45 Example 1Comparative graphite 2.3 90.00% 40 3.39 4.138 Example 2 Comparativegraphite 19 90.00% 40 0.43 14.58 Example 3 Comparative graphite 1990.00% 3.5 3.36 14.58 Example 4 Comparative graphite 15 90.00% 3.2 3.3012.08 Example 5 Comparative graphite 4 90.00% 2.5 3.17 5.20 Example 6Actual Equilibrium Processing energy Kinetic Cycle life Items constant Kperformance density performance (cycle) Example 1 0.127 Good Very highNo lithium 3450 precipitation Example 2 0.059 Good Very high No lithium3380 precipitation Example 3 0.053 Good Very high No lithium 3140precipitation Example 4 0.034 Good Very high Slight lithium 2300precipitation Example 5 0.032 Good Very high Slight lithium 2120precipitation Example 6 0.031 Good Very high Moderate lithium 1800precipitation Example 7 0.043 Good High Slight lithium 2070precipitation Example 8 0.045 Good High Slight lithium 2160precipitation Example 9 0.061 Good High Slight lithium 2370precipitation Example 10 0.063 Good High No lithium 3120 precipitationExample 11 0.109 Good High No lithium 3460 precipitation Example 120.236 Good High Slight lithium 2410 precipitation Example 13 0.591 GoodVery low Slight lithium 2370 precipitation Example 14 0.447 Good Verylow Slight lithium 2500 precipitation Example 15 0.390 Good Very low Nolithium 3420 precipitation Example 16 0.379 Good Very low No lithium3220 precipitation Example 17 0.376 Good Very low No lithium 3100precipitation Example 18 0.375 Good Very low No lithium 2980precipitation Example 19 0.699 Slightly falling Very low Slight lithium2060 off powders precipitation Example 20 0.574 Slight falling Very lowSlight lithium 2170 off powders precipitation Example 21 0.275 Good LowNo lithium 3600 precipitation Example 22 0.097 Good Moderate No lithium3440 precipitation Example 23 0.042 Good High Slight lithium 2420precipitation Example 24 0.029 Slight Very high Slight lithium 2250bumping precipitation Example 25 0.026 Serious Very high Slight lithium2040 bumping precipitation Example 26 0.036 Good High Slight lithium2200 precipitation Example 27 0.035 Good High Slight lithium 2510precipitation Example 28 0.035 Good High Slight lithium 2380precipitation Example 29 0.034 Good Very high Slight lithium 2260precipitation Example 30 0.034 Good Very high Slight lithium 2060precipitation Example 31 0.052 Good Moderate Slight lithium 2260precipitation Example 32 0.050 Good Moderate Slight lithium 2560precipitation Example 33 0.050 Good Moderate Slight lithium 2400precipitation Example 34 0.048 Good High Slight lithium 2310precipitation Example 35 0.048 Good High Slight lithium 2170precipitation Example 36 0.428 Good Very low No lithium 3110precipitation Example 37 0.402 Good Very low No lithium 3250precipitation Example 38 0.390 Good Very low No lithium 3300precipitation Example 39 0.368 Good Low No lithium 3180 precipitationExample 40 0.360 Good Low No lithium 3060 precipitation Example 41 0.268Good Low No lithium 3320 precipitation Example 42 0.303 Good Moderate Nolithium 3180 precipitation Example 43 0.113 Good Moderate No lithium3610 precipitation Example 44 0.111 Good Moderate No lithium 3570precipitation Example 45 0.328 Good Low No lithium 2980 precipitationExample 46 0.300 Good Low No lithium 3050 precipitation Example 47 0.171Good Moderate No lithium 4100 precipitation Example 48 0.197 GoodModerate No lithium 4500 precipitation Example 49 0.166 Good Moderate Nolithium 5300 precipitation Comparative 0.014 Serious Very high Seriouslithium 170 Example 1 bumping precipitation Comparative 0.820 Seriousfalling Very low Serious lithium 210 Example 2 off powders precipitationComparative 0.030 Good Very high Serious lithium 260 Example 3precipitation Comparative 0.230 Good Very high Serious lithium 450Example 4 precipitation Comparative 0.274 Good High Serious lithium 280Example 5 precipitation Comparative 0.609 Good Very low Serious lithium360 Example 6 precipitation

First, as can be seen from the data of Examples 1-49 and ComparativeExamples 1-6: In order to obtain the battery having a good fast chargeperformance (i.e. no serious lithium precipitation in the fast chargetest) while maintaining the necessary cycle performance (i.e. the numberof cycles is at least greater than 1500 times), the kinetic parameterA=7.8/D50+1.9×D50/(V_(OI))² must be kept in the range of 0.45≤A≤3.1.Specifically, as shown in Comparative Examples 1 and 3, when A<0.45,serious lithium precipitation occurs in the batteries, resulting in adramatic capacity fade (“diving phenomenon”) of cycle; Similarly, whenA>3.1, such as in Comparative Examples 2, 4, 5, and 6, serious lithiumprecipitation occurs in the batteries, resulting in a dramatic capacityfade (“diving phenomenon”) of cycle. In contrast, when A is in the rangeof 0.45≤A≤3.1, the batteries have good fast charge performance and cycleperformance. Even if in the critical region close to the boundary of therange (for example, A=0.47 in Example 5, A=0.45 in Example 6, and A=3.02in Example 19), only a moderate lithium precipitation is shown in theworst case in the battery fast charge test, meanwhile the number ofcycles is not less than 1800. When the kinetic parameter A fulfills thecondition 0.75≤A≤2.0, no lithium precipitation occurs during fastcharging and the batteries have a the number of cycles of higher than3000 times and excellent performance. Therefore, the preferred range ofA is 0.75≤A≤2.0.

In addition, in Examples 1-6, 7-12, and 13-18, the influence of varyingOI values of the negative electrode layers on the battery performancewere examined under the conditions with the fixed values of particlediameters D50 of negative electrode active material and the degree ofgraphitization G. It can be seen from these Examples that: withdifferent particle diameters D50, the influences of the OI values of thenegative electrode layers on the battery performance are not the same,and the relationship between the V_(OI) value and the fast chargeperformance of the battery is also not a simple linear relationship.When an electrode plate is designed, it is important to match the V_(OI)value of the negative electrode layer with the particle diameter D50 ofthe negative electrode material. When the V_(OI) value and the D50 valueare well matched so that the kinetic parameter A falls within apreferred range of 0.75≤A≤2.0, no lithium precipitation occurs and thebattery has an excellent cycle performance. When the V_(OI) value andthe D50 value are not matched and A falls outside the above preferredrange, slight lithium precipitation may occur in the battery.

Furthermore, it can be found by the comparison of Examples 1-18 that theenergy density parameter B=D50×0.625+G×3 is closely related to theactual energy density performance of a battery. In order to maintain ahigh energy density, the parameter B should not be lower than 5.3. InExample 13-18, the D50 is too small and the resulting B is lower than5.3, in which case the battery has relatively good fast chargeperformance and cycle performance, however, the energy density is verylow.

In Examples 19-25, the influences of different graphites as the negativeelectrode active material on the battery performance with the samedegree of graphitization G were compared, under the conditions with thesame OI value of layer. In these examples, all of the A values fallwithin the range of 0.45≤A≤3.1, the batteries have relatively good fastcharge performance and cycle performance, and no lithium precipitationor slight lithium precipitation occurs during fast charging, and all ofthe numbers of cycle are greater than 2000 times. Especially, when thekinetic parameter A fulfills the condition of 0.75≤A≤2.0 (in Examples 21and 22), the batteries have excellent performance and no lithiumprecipitation occurs during fast charging, and all of the numbers ofcycle are greater than 3000 time. In addition, it can be seen that asD50 increases, the energy density parameter B=D50×0.625+G×3 alsoincreases, and accordingly the actual energy density of the battery alsoincreases. When D50 is too small, the active ion-intercalatable sitesare less, that is, the negative electrode active material has a lowercapacity per gram and a lower battery energy density, and the badadhesion of too small particles causes the fall-off phenomenon ofpowders. From the experimental results, the energy density parameter Bshould not be less than 5.3. However, when the D50 is too large, even ifthe energy density of the battery is high, the slurry tends to settle,and bumps are likely to occur during coating with low yield, which inturn leads to poor cycle performance. Under comprehensive consideration,the energy density parameter B is preferably not greater than 14.5, morepreferably not greater than 12.

In Examples 26-40 the influences of the degrees of graphitization G onbattery performance under the conditions with varying D50 values (19,15, 4 μm) were compared, by adjusting the process to maintain a fixed OIvalue of the negative electrode layer. In these examples, all of the Avalues are in the range of 0.45≤A≤3.1, the batteries have relativelygood fast charge performance and cycle performance, and no lithiumprecipitation or slight lithium precipitation occurs during fastcharging, and all of the numbers of cycle are greater than 2000 times.Especially, when the kinetic parameter A fulfills the condition of0.75≤A≤2.0 (Examples 36-40), the batteries have excellent performancewithout lithium precipitation during fast charging and all of thenumbers of cycle are greater than 3000 times. In addition, it can beseen that as the value of the degree of graphitization G increases, theenergy density parameter B=D50×0.625+G×3 also increases, and accordinglythe actual energy density of the battery also increases. When the degreeof graphitization G is too large, the particles tend to be flat, and thestructure of pores is too dense, which is not conducive to theinfiltration of electrolyte and causes worse cycle performance ofbattery. In contrast, when the degree of graphitization G is too small,the crystals tend to have amorphous structure with many defects, and thenegative electrode active material has lower capacity per gram, which isdisadvantageous for designing a battery with high energy density.Therefore, D50 and G should be comprehensively considered, so that B hasa range of 5.3≤B≤14.5, and preferably 6.5≤B≤12. For example, in Examples36-38 where both D50 and G are small and B<5.3, the batteries have verylow actual energy density; while in Examples 29 and 30 where B>14.5, thecycle performance is relatively poor.

In Examples 41-46, the influences of the energy density parameter B andthe equilibrium constant K=A/B on the battery performance werediscussed. In these examples, all of the A values fall within the mostpreferred range of 0.75≤A≤2.0, thus the batteries have excellent fastcharge performance and cycle performance with no lithium precipitation,and the numbers of cycle are greater than 2900 times. It can be seenfrom the experimental data that, the value of the energy densityparameter B directly affects the actual energy density of the battery.In these examples, all of the B values fall within the range of5.3≤B≤14.5, and the energy densities of the batteries are finally at anacceptable level. However, when B is lower than 6.5 (Examples 41, 45,and 46), the batteries have relative low energy density. Undercomprehensive consideration with the range of B values in otherExamples, the most preferred range of B is 6.5≤B≤12.

In addition, Examples 41-46 further illustrate the influence of theequilibrium constant K=A/B on the battery performance. It can be seenfrom the test data that when 0.055≤K≤0.31 (Examples 41-44), thebatteries have relative good fast charge performance, cycle performance,and energy density. Especially when 0.112≤K≤0.26 (Examples 43), thebatteries have best performance.

Examples 1-46 show the examples in which graphite material is used asthe negative electrode active material to illustrate the technicalsolutions and effects of the present disclosure. Examples 47-49 showanother embodiment of the present disclosure in which a mixed materialcomprising a graphite material is used as the negative electrode activematerial. In Examples 47-49 where graphite material and other commonlyused negative electrode active materials (soft carbon, hard carbon,lithium titanate) were mixed as negative electrode active material whilemaintaining the kinetic parameter A in the most preferred range of0.75≤A≤2.0, and the energy density parameter B in the most preferredrange of 6.5≤B≤12, and the equilibrium constant K in the most preferredrange of 0.112≤K≤0.26, the results show that the batteries in therespective examples have very excellent processing performance, cycleperformance (greater than 4000 time), fast charge performance (nolithium precipitation) and energy density. This indicates, theparameters A, B, and K as defined in the disclosure are also applicableto the mixed negative electrode active material comprising graphitematerial.

It is also to be understood that the above-described embodiments may beappropriately modified and varied by those skilled in the art in lightof the above disclosure. Therefore, the present invention is not limitedto the specific embodiments as disclosed and described above, and themodifications and variations of the disclosure are intended to fallwithin the scope of the appended claims. In addition, although somespecifically defined terms are used in the specification, these termsare merely used for convenience of description and do not impose anylimitation on the present invention.

What is claimed is:
 1. A secondary battery, comprising a negativeelectrode plate, the negative electrode plate comprises a negativeelectrode current collector and a negative electrode layer coated on atleast one surface of the negative electrode current collector, thenegative electrode layer comprising a negative electrode activematerial, wherein the negative electrode active material comprises agraphite material, and the negative electrode layer fulfills thecondition:0.75≤7.8/D50+1.9×D50/(V _(OI))²≤2.0 Wherein D50 represents a volumedistribution average particle diameter of particles of the negativeelectrode active material in micron, V_(OI) represents the OI value ofthe negative electrode layer, and V_(OI)=C₀₀₄/C₁₁₀, wherein C₀₀₄ was thepeak area of the 004 characteristic diffraction peak, and C₁₁₀ is thepeak area of the 110 characteristic diffraction peak in X-raydiffraction spectrum of the negative electrode plate, and wherein thevolume distribution average particle diameter D50 of the negativeelectrode active material is 4-15 μm.
 2. The secondary battery accordingto claim 1, wherein the negative electrode layer fulfills the condition:0.75≤7.8/D50+1.9×D50/(V _(OI))²≤1.31.
 3. The secondary battery accordingto claim 1, wherein the negative electrode active material fulfills thecondition:6.5≤D50×0.625+G×3≤12 wherein D50 represents a volume distributionaverage particle diameter of particles of the negative electrode activematerial in micron, G represents the degree of graphitization of thenegative electrode active material.
 4. The secondary battery accordingto claim 3, wherein the negative electrode active material fulfills thecondition:8.95≤D50×0.625+G×3≤11.45.
 5. The secondary battery according to claim 1,wherein the negative electrode layer fulfills the condition:0.055≤A/B≤0.31 wherein A=7.8/D50+1.9×D50/(V_(OI))²B=D50×0.625+G×3 D50 represents a volume distribution average particlediameter of particles of the negative electrode active material inmicron, V_(OI) represents the OI value of the negative electrode layer,G represents the degree of graphitization of the negative electrodeactive material.
 6. The secondary battery according to claim 5, whereinthe negative electrode layer fulfills the condition:0.061≤A/B≤0.097.
 7. The secondary battery according to claim 1, whereinthe volume distribution average particle diameter D50 of the negativeelectrode active material is 5-15 μm.
 8. The secondary battery accordingto claim 1, wherein the volume distribution average particle diameterD50 of the negative electrode active material is 10-15 μm.
 9. Thesecondary battery according to claim 1, wherein the OI value V_(OI) ofthe negative electrode layer is 1.5-50.
 10. The secondary batteryaccording to claim 1, wherein the OI value V_(OI) of the negativeelectrode layer is 6-20.
 11. The secondary battery according to claim 1,wherein the OI value V_(OI) of the negative electrode layer is 15-20.12. The secondary battery according to claim 1, wherein the degree ofgraphitization G of the negative electrode active material is 80%-98%.13. The secondary battery according to claim 12, wherein the degree ofgraphitization G of the negative electrode active material is 90%-95%.14. The secondary battery according to claim 1, wherein the powder OIvalue G_(OI) of the negative electrode active material is 2-4.5.
 15. Thesecondary battery according to claim 1, wherein the press density PD ofthe negative electrode layer is 1.0 g/cm³-1.6 g/cm³.
 16. The secondarybattery according to claim 1, wherein the graphite material comprisesartificial graphite.
 17. The secondary battery according to claim 1,wherein the secondary battery comprises a positive electrode plate, thepositive electrode plate comprises a positive electrode currentcollector and a positive electrode layer disposed on the surface of thepositive electrode current collector, the positive electrode layercomprises a positive electrode active material, and the positiveelectrode active material comprises lithium nickel cobalt manganeseoxide.